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A flat panel display apparatus with a mounting apparatus includes a display screen, a handle member, a supporting member and a stand member. The handle member is disposed at the edge or the rear of the display screen. The supporting member is pivotally secured to the handle member. The supporting me

A flat panel display apparatus with a mounting apparatus includes a display screen, a handle member, a supporting member and a stand member. The handle member is disposed at the edge or the rear of the display screen. The supporting member is pivotally secured to the handle member. The supporting member has a first arm portion and a second arm portion where an obtuse angle is formed between the first arm portion and the second arm portion. The stand member is disposed at an end of the second arm portion to provide friction between the second arm portion and contacted surface thereon and prevent the second arm portion from escaping as the display screen is in an upright position.

대표청구항 ▼

A flat panel display apparatus with a mounting apparatus includes a display screen, a handle member, a supporting member and a stand member. The handle member is disposed at the edge or the rear of the display screen. The supporting member is pivotally secured to the handle member. The supporting me

A flat panel display apparatus with a mounting apparatus includes a display screen, a handle member, a supporting member and a stand member. The handle member is disposed at the edge or the rear of the display screen. The supporting member is pivotally secured to the handle member. The supporting member has a first arm portion and a second arm portion where an obtuse angle is formed between the first arm portion and the second arm portion. The stand member is disposed at an end of the second arm portion to provide friction between the second arm portion and contacted surface thereon and prevent the second arm portion from escaping as the display screen is in an upright position. im 1, further comprising: means for biasing each of said plurality of solar panels toward said deployed position. 15. A satellite assembly, as claimed in claim 14, wherein: said means for biasing comprises a separate spring for each of said plurality of solar panels. 16. A satellite assembly, as claimed in claim 1, further comprising: a separate deployment spring for each of said plurality of solar panels. 17. A satellite assembly, as claimed in claim 1, further comprising: means for pivoting each of said plurality of solar panels from said stored position to said deployed position while maintaining each of said plurality of solar panels in parallel relation to each other throughout movement from said stored position to said deployed position. 18. A method for operating a satellite assembly comprising a first solar panel, a second solar panel, a third solar panel, and a fourth solar panel, said method comprising the steps of: maintaining said plurality of solar panels in a stored position; moving said plurality of solar panels from said stored position to a deployed position, wherein said moving step comprises pivoting said first and second solar panels about a first axis, in opposite directions, and in first and second reference planes, and pivoting said third and fourth solar panels about a second axis, in opposite directions, and in third and fourth reference planes, wherein said first and second reference planes are vertically offset and parallel to each other, and wherein said third and fourth reference planes are vertically offset and parallel to each other. 19. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in parallel relation. 20. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in stacked relation. 21. A satellite assembly, as claimed in claim 18, wherein: said maintaining step comprises disposing said plurality of solar panels in both a parallel and stacked relation. 22. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are parallel to each other. 23. A satellite assembly, as claimed in claim 18, wherein: said first, second, third, and fourth reference planes are vertically offset and parallel to each other. 24. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are parallel to each other, and wherein said first, second, third, and fourth reference planes are vertically offset and parallel to each other. 25. A satellite assembly, as claimed in claim 18, wherein: said moving step comprises pivoting said first, second, third, and fourth, solar panels along parallel paths throughout said moving step. 26. A satellite assembly, as claimed in claim 18, wherein: said first and second axes are 180 degrees apart. 27. A satellite assembly, as claimed in claim 18, further comprising: means for pivoting said first and second solar panels about said first connector in opposite directions from said stored position to said deployed position; and means for pivoting said third and fourth solar panels about said second connector in opposite directions from said stored position to said deployed position, wherein said first and second connectors are parallel to each other. 28. A method for operating a satellite assembly comprising a plurality of solar panels, said method comprising the steps of: disposing said plurality of solar panels in a store position, wherein said disposing step comprises disposing said plurality of solar panels in a stack such that each of said plurality of solar panels is at a different elevation within said stack and such that said plurality of solar panels are in parallel relation within said stack; deploying said plurality of solar panels from said stored position to a deployed position, wherein said deploying step